The influence of neighboring blade rows on the unsteady aerodynamic response of cascades

Published

Conference Paper

Copyright © 1995 by ASME All Rights Reserved. In this paper, we present an analysis of the unsteady aerodynamic response of cascades due to incident gusts (the forced response problem) or blade vibration (the flutter problem) when the cascade is part of a multistage fan, compressor, or turbine. Most current unsteady aerodynamic models assume the cascade to be isolated in an infinitely long duct. This assumption, however, neglects the potentially important influence of neighboring blade rows. We present an elegant and computationally efficient method to model these neighboring blade row effects. In the present method, we model the unsteady aerodynamic response due to so-called spinning modes (pressure and vorticity waves), with each mode corresponding to a different circumferential wave number and frequency. Then, for each mode, we compute the reflection and transmission coefficients for each blade row. These coefficients can be obtained from any of the currently available unsteady linearized aerodynamic models of isolated cascades. A set of linear equations is then constructed that couples together the various spinning modes, and the linear equations are solved via LU decomposition. Numerical results are presented for both the gust response and blade vibration problems. To validate our model, we compare our results to other analytical models, and to a multistage vortex lattice model. We show that the effect of neighboring blade rows on the aerodynamic damping of vibrating cascades is significant, but nevertheless can be modeled with a small number of modes.

Full Text

Duke Authors

Cited Authors

  • Hall, KC; Silkowski, PD

Published Date

  • January 1, 1995

Published In

  • Proceedings of the Asme Turbo Expo

Volume / Issue

  • 1 /

International Standard Book Number 13 (ISBN-13)

  • 9780791878781

Digital Object Identifier (DOI)

  • 10.1115/95-GT-035

Citation Source

  • Scopus